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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in gas turbines, is of

None of the listed here
Radial flow type
Axial flow type
Centrifugal type

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Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Compression work/motor input
Total output/air input
Isothermal H.P/indicated H.R
Isothermal H.P./shaft H.R

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Compressors, Gas Turbines and Jet Engines
The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is

Same
May be less or more depending on ambient conditions
More
Less

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Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

Stainless steel
High alloy steel
Carbon steel
High nickel alloy

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Compressors, Gas Turbines and Jet Engines
Diffuser in a compressor is used to

Increase velocity
Convert kinetic energy into pressure energy
Make the flow streamline
Convert pressure energy into kinetic energy

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

All of these
Higher volumetric efficiency
Lower power consumption per unit of air delivered
Decreased discharge temperature

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